N170UP

Service difficulty reports · 151

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N170UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2016082107280Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POSITION 1 AFT LEFT CORNER DAMAGED. REPAIRED IAW SRM 53-10-20-201 PARA 8A.Aug 21, 2016 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2016070705523Skin · damagedDAMAGE TO FUSELAGE SKIN AT FRAME 6. REPAIRED IAW EO A300-5330-61180-A.Jul 3, 2016 · N170UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2016070705522Frame · damagedDAMAGE TO FRAME 6 AT F.O.'S PITOT PROBE. REPAIRED IAW EO A300-5310-61181-AJul 3, 2016 · N170UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2015092994074Connector · dirtyCOURIER EMERGENCY LIGHT TEST FUNCTION INOPERATIVE. CLEANED CONNECTOR AT 29WLI POWER SUPPLY UNIT. RESEATED AND OPS CHECKED GOOD IAW AMM 33-51-00-0501.Sep 28, 2015 · N170UP · Airbus A300F4622R · Light System WiringSDR IPXA2015080592051Window Frame · gougedINSPECTION TYPE: 10 YEAR, EXTERNAL FUSELAGE AT RT SIDE WINDSHIELD LOWER INBD CUTOUT GOUGED. REPAIRED IAW REO-G19090, REV A AND EO A300-5310-58294-A.Jul 19, 2015 · N170UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2015080892153Stiffener · crackedINSPECTION TYPE:10YR, AFT CARGO AT FWD BULKHEAD FRAME 54 AND RBL 77 ABOVE WING BOX VERTICAL STIFFENER IS CRACKED. R & R STIFFENER,IAW SRM 51-40-21.Jul 18, 2015 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2015080592043Floor Panel · crackedINSPECTION TYPE: 10 YEAR, MAIN CABIN FLOOR PANEL FOUND CRACKED. REPAIRED THE FLOOR PANEL IAW EO A300-5320-42721F.Jul 18, 2015 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2015072791587Floor Panel · damagedINSPECTION TYPE:10YR, SUPERNUMERARY FLOOR PANEL 221VF HAS EDGE DAMAGE, FABRICATED FLOOR PANEL IAW EO A300-5320-40552-B.Jul 17, 2015 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2015080592052Angle · crackedINSPECTION TYPE: 5 YEAR, NR 2 PYLON LT AFT LOWER ANGLE CRACKED. R & R ANGLE WITH NEW.Jul 16, 2015 · N170UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2015080592058Stiffener · crackedINSPECTION TYPE: 10 YEAR, AFT CARGO AT FWD BULKHEAD FRAME 54 AND LBL 38.5 VERTICAL STIFFENER IS CRACKED. R & R THE STIFFENER.Jul 16, 2015 · N170UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2015080592057Stiffener · crackedDURING ACFT 10 YEAR MAINTENANCE VISIT, AFT CARGO BAY FWD BULKHEAD VERTICAL STIFFENER AT FRAME 54, BL 0 WAS FOUND TO BE CRACKED BEYOND SRM LIMITS. R & R STIFFENER.Jul 16, 2015 · N170UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2015081092217Failsafe · dentedINSPECTION TYPE:10YR, CREW ENTRY DOOR FAIL SAFE RING HAS A DENT AT THE FWD UPPER AREA. REMOVED FASTENERS AND HFEC HOLES IAW EO A300-5330--58295-A.Jul 15, 2015 · N170UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2015080892152Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131MG HAS 11 PUNCTURES ON BOTTOM SIDE. REPAIRED THE FLOOR PANEL IAW SRM 53-10-20, PARA 8.B, FIG 203, SHEET 2.Jul 15, 2015 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2015072991718Floorbeam · crackedINSPECTION TYPE: 10Y, MAIN CABIN UNDER FLOORBEAM ANGLE FRAME 79, Y 1589 IS CRACKED. FABRICATED AND INSTALLED A NEW ANGLE IAW 5310-58113-A.Jul 15, 2015 · N170UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2015072391468Lug · crackedINSPECTION TYPE:10YR, NR 1 THRUST REVERSER LOWER OTBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVED. HOLE SIZE AT .748, REAMED HOLE TO .7772 IAW EO A300-7830-19599-Z, STEP 12K.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391467Lug · crackedINSPECTION TYPE: 10YR, NR 1 THRUST REVERSER UPPER OTBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVED. HOLE SIZE AT .748, REAMED HOLE TO .7772 IAW EO A300-7830-19599-Z, STEP 12K.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391477Lug · crackedINSPECTION TYPE:10YR, NR 2 THRUST REVERSER LOWER OTBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVAL. HOLE AT .687 PERFORMED FINAL REAM OF LUG FOR NEXT ALLOWABLE BEARING. HOLE SIZE IS .7472, IAW A300-7830-19599-Z.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391476Lug · crackedINSPECTION TYPE: 10YR, NR 1 THRUST REVERSER LOWER INBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVAL. HOLE AT .687 REAMED HOLE TO NEXT ALLOWABLE OVERSIZE BEARING . FINAL HOLE SIZE IS .7072, IAW A300-7830-19559-Z.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391475Lug · crackedINSPECTION TYPE:10YR, NR 1 THRUST REVERSER UPPER INBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVAL. HOLE AT .687 REAMED T/R LUG TO .747 IAW A300-7830-19599-Z, APPENDIX C, STEP K.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391474Lug · crackedINSPECTION TYPE:10YR, NR 2 THRUST REVERSER LOWER INBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVED. HOLE SIZE AT .648, REAMED LUG TO .7472, REV A300-7830-19599-Z, APPENDIX D, STEP K.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391473Lug · crackedINSPECTION TYPE: 10YR, NR 2 THRUST REVERSER UPPER INBD TRACK LUG HAS CRACK INDICATION AFTER BEARING REMOVED. HOLE SIZE AT .648. REAMED NR 2 T/R INBD UPPER LUG TO .7472, IAW A300-7830-19599-Z APPENDIX D, STEP K.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015072391478Lug · crackedINSPECTION TYPE: 10YR, NR 2 THRUST REVERSER UPPER OTBD TRACK LUG HAS A CRACK INDICATION AFTER BEARING REMOVAL. HOLE AT .687. PERFORMED FINAL REAM OF LUG FOR NEXT ALLOWABLE BEARING. HOLE SIZE IS .7472, IAW A300-7830-19599-Z.Jul 15, 2015 · N170UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2015071491162Floorbeam · crackedINSPECTION TYPE:10YR, MAIN CABIN FLOORBEAM, FRAME 79 L 1580 IS CRACKED. REPAIRED IAW EO A300-5310-58053-A.Jul 12, 2015 · N170UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2015071491161Floorbeam · crackedINSPECTION TYPE:10YR, MAIN CABIN FLOOR CROSSBEAM FRAME 79, RT -Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-58053-A.Jul 12, 2015 · N170UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2015032787465Light · inoperativeLAV AUX/MIRROR LIGHT INOPERATIVE RELAMPED REF AMM33-51-21-401.Mar 27, 2015 · N170UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2014082084025Bulb · inoperativeONE LAMP IN EMERGENCY LIGHT SYS INOPERATIVE. REPLACED THE BULB. OPS CHECKED OK IAW AMM 33-12-00-0901.Aug 15, 2014 · N170UP · Airbus A300F4622R · Emergency LightingSDR IPXA201407023470Cover · unsecureF/O'S ESCAPE ROPE COVER WILL NOT STAY SECURED. SECURED F/O EMERGENCY ESCAPE ROPE IAW AMM 25-61-13 AND BLOCK 401. NO FURTHER DEFECTS NOTED AT THIS TIME.Jun 29, 2014 · N170UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2014182569Skin · dentedLT FUSELAGE SKIN SIDE PANEL DENTED AT FRAME 3 AND FRAME 4 BELOW UPPER LAP SPLICE. REPAIRED IAW EO A300-5330-37157-B.Apr 7, 2014 · N170UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2013111500849Bulb · inoperativeLAVATORY MIRROR LIGHT INOPERATIVE, REPLACED BULB.Nov 14, 2013 · N170UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA13177525Skin · damagedINSPECTION TYPE:3C, LOWER FUSELAGE EXTERNAL SKIN AROUND TAIL STAND FITTING AT FR 85 BETWEEN STGR 44L AND STGR 43R HAS A DENT AND GOUGE MARK ACCOMPLISHED REPAIR ON LOWER FUSELAGE SKIN AROUND TAIL STAND FITTING AT FR 85 IAW SRM 53-10-12, FIG 210, REV 23.Mar 4, 2013 · N170UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA3176770Skin · dentedFUSELAGE SKIN DENTED BETWEEN FR 12 + 12A ABOVE S25R. REPAIRED IAW EO A300--5330-36569-C.Jan 21, 2013 · N170UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA12175611Girt Bar · out of positionAFTER LANDING, WHEN TRYING TO DISARM ESCAPE SLIDE HANDLE DOESN`T COME TOO FAR LEFT, ECAM SHOWS SLIDE DISARMED TRIGS AGAIN THE HANDLE WENT FULL LEFT AND OPENED THE DOOR WITH NO OTHER PROBLEMS. FWD GIRT BAR SLIDER HITTING LIFTING HOOK WHEN DISARMING. TRIED NEWSep 28, 2012 · N170UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA12175610Girt Bar · unsecureWHEN TRYING TO OPEN DOOR, NOT GETTING DISARMING LEVER TO FULL LT SIDE. ECAM SHOWED SLIDE DISARMED. OPENED DOOR SLIDE DID NOT DEPLOY, BUT GIRT BAR WAS DETACHED. FOUND GIRT BAR NOT SECURED ON FWD DOOR SLIDE TRACK. SECURED GIRT BAR, DOOR OPS NORMAL THRU SEVESep 27, 2012 · N170UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2175533Girt Bar · lack of lubeEMERGENCY EXIT SLIDE VERY DIFFICULT TO DISARM. LUBRICATED GIRT BAR IAW MM 12-22-52. OPS CK NORMAL.Sep 20, 2012 · N170UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2175195Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231PH HAS EDGE DAMAGE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175203Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231KJ HAS EDGE DAMAGE. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175194Floorboard · puncturedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231LG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175190Floorboard · damagedINSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231RH HAS EDGE DAMAGE. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175189Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232LT HAS LOWER SKIN EDGE DAMAGE FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175188Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 221EG HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175187Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222CG HAS CORRODED INSERTS AND LOWER SKIN IS DAMAGED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175185Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222DG LOWER SKIN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175186Floorboard · puncturedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232LF LOWER SKIN IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 3, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12172742Control Module · inoperativeAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. HANDLE MOVED TO UP POSITION GEAR INDICATION SHOWED GREEN DOWN WITH UNLOCK LIGHT SYS 1 & 2. AIR TURN BACK. R & R LANDING GEAR CONTROL MODULE HANDLE IAW MM 32-31-11-04. PS CHECK OK.Apr 2, 2012 · N170UP · Airbus A300F4622R · Landing Gear SelectorSDR IPXA2172636Floorboard · damagedFLOORBOARD DAMAGED FWD LOWER PIT RT INBD SIDE. FABRICATED NEW FLOORBOARD IAW EO A300-5330-16407-E.Mar 27, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1168591Light · inoperativeSEVERAL DOOR EXIT SIGN LAMPS INOPERATIVE. RELAMPED AND TEST NORMAL IAW AMM 33-51-13-04.Aug 11, 2011 · N170UP · Airbus A300F4622R · Emergency LightingSDR IPXA10163456Floor Panel · crackedINSPECTION TYPE:5 YR, FLOOR PANEL 232FFIS CRACKED AT LOWER SURFACE AS MARKED. FABRICATED MAIN DECK FLOOR PANEL 232FF REF EO A300-5320-16407, APPX A AND B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163455Floor Panel · delaminatedINSPECTION TYPE:5YR, FLOOR PANEL 231KJ DELAMINATED. FABRICATED MAIN DECK FLOOR PANEL 231KJ REF EO A300-5320-16407, APPX A AND B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163438Floor Panel · crackedINSPECTION TYPE:5 YR, FWD PIT FLOORBOARD PANEL 131BH HAS A CRACK. FABRICATED LOWER, FWD CARGO COMPT FLOOR PANEL 131BH REF EO A300-5320-16407-E APPX A AND C.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163436Floor Panel · delaminatedINSP TYPE:5 YR MCD FLOOR PANEL 231GH DELAMINATED. FABRICATED MAIN CARGO DECK FLOOR PANEL 231GH REF EO A300-5320- 16407-E APPX A AND B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
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